View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 27842U 03031C 23271.56413084 .00000480 00000-0 23319-3 0 9999
2 27842 98.6896 276.5050 0009784 154.4476 205.7187 14.22784190 50604
| Epoch (UTC): | 28 September 2023 13:32:20 |
| Eccentricity: | 0.0009784 |
| inclination: | 98.6896° |
| perigee height: | 809 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 276.5050° |
| argument of perigee: | 154.4476° |
| revolutions per day: | 14.22784190 |
| mean anomaly at epoch: | 205.7187° |
| orbit number at epoch: | 5060 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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